JP6641496B2 - リアクション補償式ステアリング可能プラットフォーム - Google Patents

リアクション補償式ステアリング可能プラットフォーム Download PDF

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Publication number
JP6641496B2
JP6641496B2 JP2018544124A JP2018544124A JP6641496B2 JP 6641496 B2 JP6641496 B2 JP 6641496B2 JP 2018544124 A JP2018544124 A JP 2018544124A JP 2018544124 A JP2018544124 A JP 2018544124A JP 6641496 B2 JP6641496 B2 JP 6641496B2
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JP
Japan
Prior art keywords
base
steerable platform
reaction
reaction mass
steerable
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
JP2018544124A
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English (en)
Japanese (ja)
Other versions
JP2019514036A (ja
Inventor
エル． バラッド，アンドリュー
エル． バラッド，アンドリュー
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Co
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Raytheon Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Application filed by Raytheon Co filed Critical Raytheon Co
Publication of JP2019514036A publication Critical patent/JP2019514036A/ja
Application granted granted Critical
Publication of JP6641496B2 publication Critical patent/JP6641496B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/64—Imaging systems using optical elements for stabilisation of the lateral and angular position of the image
    • G02B27/644—Imaging systems using optical elements for stabilisation of the lateral and angular position of the image compensating for large deviations, e.g. maintaining a fixed line of sight while a vehicle on which the system is mounted changes course
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244—Spacecraft control systems
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B26/00—Optical devices or arrangements for the control of light using movable or deformable optical elements
    • G02B26/08—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light
    • G02B26/0816—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light by means of one or more reflecting elements
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B7/00—Mountings, adjusting means, or light-tight connections, for optical elements
    • G02B7/18—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors
    • G02B7/182—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors
    • G02B7/1822—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors comprising means for aligning the optical axis
    • G02B7/1827—Motorised alignment
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K41/00—Propulsion systems in which a rigid body is moved along a path due to dynamo-electric interaction between the body and a magnetic field travelling along the path
    • H02K41/02—Linear motors; Sectional motors
    • H02K41/035—DC motors; Unipolar motors
    • H02K41/0352—Unipolar motors
    • H02K41/0354—Lorentz force motors, e.g. voice coil motors
JP2018544124A 2016-02-22 2016-12-22 リアクション補償式ステアリング可能プラットフォーム Expired - Fee Related JP6641496B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US15/050,359 US10197792B2 (en) 2016-02-22 2016-02-22 Reaction compensated steerable platform
US15/050,359 2016-02-22
PCT/US2016/068345 WO2017146812A1 (en) 2016-02-22 2016-12-22 Reaction compensated steerable platform

Publications (2)

Publication Number Publication Date
JP2019514036A JP2019514036A (ja) 2019-05-30
JP6641496B2 true JP6641496B2 (ja) 2020-02-05

Family

ID=57838495

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2018544124A Expired - Fee Related JP6641496B2 (ja) 2016-02-22 2016-12-22 リアクション補償式ステアリング可能プラットフォーム

Country Status (5)

Country Link
US (1) US10197792B2 (en.)
EP (1) EP3420399A1 (en.)
JP (1) JP6641496B2 (en.)
IL (1) IL261177B (en.)
WO (1) WO2017146812A1 (en.)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11852803B2 (en) 2020-10-28 2023-12-26 Raytheon Company Large aperture, single axis, reactionless fast steering mirror
CN114952744B (zh) * 2022-07-05 2022-12-20 广东工业大学 一种音圈电机直驱式主动隔振调平一体化平台

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1272565B (de) 1965-05-11 1968-07-11 Bundesrep Deutschland Anordnung zur raumfesten Stabilisierung von Geraeten auf Fahrzeugen
FR2642538B1 (fr) 1989-01-31 1991-05-24 Europ Propulsion Systeme de stabilisation mecanique a contre-rotation a rotors emboites
US5283682A (en) 1992-10-06 1994-02-01 Ball Corporation Reactionless scanning and positioning system
US5751078A (en) 1996-10-03 1998-05-12 Lockheed Martin Corp. Missiles & Space Reactionless, momentum compensated payload positioner
US6724466B2 (en) 2002-03-26 2004-04-20 Nikon Corporation Stage assembly including a damping assembly
US7009752B1 (en) * 2003-01-21 2006-03-07 Lockheed Martin Corporation Actively-supported multi-degree of freedom steerable mirror apparatus and method
US7898204B2 (en) * 2007-01-05 2011-03-01 Active Precision, Inc. High-speed substrate manipulator
DE102011006024A1 (de) 2011-03-24 2012-09-27 Carl Zeiss Smt Gmbh Anordnung zur Vibrationsisolation einer Nutzlast
JP6152001B2 (ja) * 2012-08-03 2017-06-21 キヤノン株式会社 アクティブ除振装置、除振方法、加工装置、検査装置、露光装置及びワークの製造方法
US9658427B2 (en) * 2013-03-15 2017-05-23 Raytheon Company Reaction compensated tilt platform

Also Published As

Publication number Publication date
EP3420399A1 (en) 2019-01-02
US20170242243A1 (en) 2017-08-24
IL261177A (en) 2018-10-31
JP2019514036A (ja) 2019-05-30
IL261177B (en) 2019-05-30
US10197792B2 (en) 2019-02-05
WO2017146812A1 (en) 2017-08-31

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